A method to determine a bound of structural loads for a spacecraft mounted on a launch vehicle is developed. The method utilizes the interface shock spectra and the relative impedance of the spacecraft and launch vehicle. The method is developed for single-degree-of-freedom models and then generalized to multidegree-of-freedom models. (Author)
A Shock Spectra and Impedance Method to Determine a Bound for Spacecraft Structural Loads
1974
42 pages
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Keine Angabe
Englisch